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contributor authorMcIntyre, Rory
contributor authorSavory, Eric
contributor authorWu, Hao
contributor authorTing, David S.-K.
date accessioned2019-03-17T10:53:54Z
date available2019-03-17T10:53:54Z
date copyright11/16/2018 12:00:00 AM
date issued2019
identifier issn0098-2202
identifier otherfe_141_05_051106.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4256376
description abstractThe effect of the nozzle top lip thickness on a two-dimensional wall jet was examined experimentally in a wind tunnel using hot-wire anemometry. Lip thicknesses of 0.125b, 0.5b, 1b, and 2b, where b is the jet nozzle height, were considered at a Reynolds number of 30,700 based on the jet nozzle height and jet velocity. Noticeable differences in the flow profiles were observed at the jet outlet, but by 10b downstream these differences became insignificant. Different lip thicknesses resulted in different maximum velocity decay rates. The spread of the wall jet was found to be insensitive to the lip thickness.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Effect of the Nozzle Top Lip Thickness on a Two-Dimensional Wall Jet
typeJournal Paper
journal volume141
journal issue5
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.4041560
journal fristpage51106
journal lastpage051106-9
treeJournal of Fluids Engineering:;2019:;volume( 141 ):;issue: 005
contenttypeFulltext


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